In this paper, the missile guidance with terminal impact Angle constraint and integratedguidance and control design for missile with terminal impact constraint were researched.
在这一背景下，本文研究了带末端攻击角度约束的制导方法设计和制导控制一体化方法设计问题。
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Considering the limitation of the anti-radiation submissile, this paper shows a method by GNSS/SINS integratedguidance to improve the hit accuracy on conditions that radar swiching-off.
A comprehensive solution will include integrated support for process guidance, requirements management, software asset management, defect and change tracking, test management, and common reporting.